CN1936279B - 用于控制燃气轮机间隙的装置 - Google Patents

用于控制燃气轮机间隙的装置 Download PDF

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Publication number
CN1936279B
CN1936279B CN2006101397644A CN200610139764A CN1936279B CN 1936279 B CN1936279 B CN 1936279B CN 2006101397644 A CN2006101397644 A CN 2006101397644A CN 200610139764 A CN200610139764 A CN 200610139764A CN 1936279 B CN1936279 B CN 1936279B
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China
Prior art keywords
housing
turbine
wall
support
ring
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CN2006101397644A
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English (en)
Chinese (zh)
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CN1936279A (zh
Inventor
弗兰克·丹内斯
文森特·菲利波特
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Safran Aircraft Engines SAS
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SNECMA SAS
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Publication of CN1936279A publication Critical patent/CN1936279A/zh
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CN2006101397644A 2005-09-23 2006-09-22 用于控制燃气轮机间隙的装置 Active CN1936279B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0509749 2005-09-23
FR0509749A FR2891300A1 (fr) 2005-09-23 2005-09-23 Dispositif de controle de jeu dans une turbine a gaz

Publications (2)

Publication Number Publication Date
CN1936279A CN1936279A (zh) 2007-03-28
CN1936279B true CN1936279B (zh) 2011-06-29

Family

ID=36600208

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2006101397644A Active CN1936279B (zh) 2005-09-23 2006-09-22 用于控制燃气轮机间隙的装置

Country Status (8)

Country Link
US (1) US7641442B2 (fr)
EP (1) EP1775427B1 (fr)
JP (1) JP4990586B2 (fr)
CN (1) CN1936279B (fr)
CA (1) CA2560227C (fr)
DE (1) DE602006003502D1 (fr)
FR (1) FR2891300A1 (fr)
RU (1) RU2435039C2 (fr)

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US7721433B2 (en) * 2005-03-28 2010-05-25 United Technologies Corporation Blade outer seal assembly
CN101952557A (zh) * 2008-03-31 2011-01-19 三菱重工业株式会社 回转机械
EP2184445A1 (fr) * 2008-11-05 2010-05-12 Siemens Aktiengesellschaft Support d'aubes statorique axialement segmenté d'une turbine à gaz
US20110103939A1 (en) * 2009-10-30 2011-05-05 General Electric Company Turbine rotor blade tip and shroud clearance control
FR2979662B1 (fr) * 2011-09-07 2013-09-27 Snecma Procede de fabrication d'un secteur de distributeur de turbine ou redresseur de compresseur en materiau composite pour turbomachine et turbine ou compresseur incorporant un distributeur ou un redresseur forme de tels secteurs
US9010127B2 (en) * 2012-03-02 2015-04-21 General Electric Company Transition piece aft frame assembly having a heat shield
RU2490474C1 (ru) * 2012-04-16 2013-08-20 Николай Борисович Болотин Турбина газотурбинного двигателя
RU2499892C1 (ru) * 2012-04-24 2013-11-27 Николай Борисович Болотин Турбина газотурбинного двигателя
RU2500894C1 (ru) * 2012-04-27 2013-12-10 Николай Борисович Болотин Турбина газотурбинного двигателя
RU2506435C2 (ru) * 2012-05-11 2014-02-10 Николай Борисович Болотин Газотурбинный двигатель и способ регулирования радиального зазора в турбине газотурбинного двигателя
RU2499894C1 (ru) * 2012-05-11 2013-11-27 Николай Борисович Болотин Двухконтурный газотурбинный двигатель
RU2501956C1 (ru) * 2012-07-31 2013-12-20 Николай Борисович Болотин Двухконтурный газотурбинный двигатель, способ регулирования радиального зазора в турбине двухконтурного газотурбинного двигателя
RU2511860C1 (ru) * 2012-09-10 2014-04-10 Николай Борисович Болотин Двухконтурный газотурбинный двигатель и способ регулирования радиального зазора в турбине двухконтурного газотурбинного двигателя
US9091171B2 (en) * 2012-10-30 2015-07-28 Siemens Aktiengesellschaft Temperature control within a cavity of a turbine engine
CA2896500A1 (fr) * 2013-01-29 2014-08-07 Rolls-Royce Corporation Enveloppe de turbine
US10094233B2 (en) 2013-03-13 2018-10-09 Rolls-Royce Corporation Turbine shroud
RU2519127C1 (ru) * 2013-04-24 2014-06-10 Николай Борисович Болотин Турбина газотурбинного двигателя и способ регулирования радиального зазора в турбине
JP5889266B2 (ja) * 2013-11-14 2016-03-22 三菱重工業株式会社 タービン
US9598981B2 (en) * 2013-11-22 2017-03-21 Siemens Energy, Inc. Industrial gas turbine exhaust system diffuser inlet lip
JP6441611B2 (ja) * 2014-08-25 2018-12-19 三菱日立パワーシステムズ株式会社 ガスタービンの排気部材及び排気室メンテナンス方法
US10190434B2 (en) 2014-10-29 2019-01-29 Rolls-Royce North American Technologies Inc. Turbine shroud with locating inserts
CA2915246A1 (fr) 2014-12-23 2016-06-23 Rolls-Royce Corporation Enveloppe de turbine
CA2915370A1 (fr) 2014-12-23 2016-06-23 Rolls-Royce Corporation Chemin de pale circulaire comportant des elements clavetes axialement
EP3045674B1 (fr) 2015-01-15 2018-11-21 Rolls-Royce Corporation Enveloppe de turbine avec inserts tubulaires de localisation de patins
US10215099B2 (en) * 2015-02-06 2019-02-26 United Technologies Corporation System and method for limiting movement of a retainer ring of a gas turbine engine
CA2924855A1 (fr) 2015-04-29 2016-10-29 Rolls-Royce Corporation Sillage de pale a distorsion trapezoidale
CA2925588A1 (fr) 2015-04-29 2016-10-29 Rolls-Royce Corporation Sillage de pale brase destine a une turbine a gaz
US10240476B2 (en) 2016-01-19 2019-03-26 Rolls-Royce North American Technologies Inc. Full hoop blade track with interstage cooling air
US10287906B2 (en) 2016-05-24 2019-05-14 Rolls-Royce North American Technologies Inc. Turbine shroud with full hoop ceramic matrix composite blade track and seal system
US10415415B2 (en) 2016-07-22 2019-09-17 Rolls-Royce North American Technologies Inc. Turbine shroud with forward case and full hoop blade track
FR3079874B1 (fr) * 2018-04-09 2020-03-13 Safran Aircraft Engines Dispositif de refroidissement pour une turbine d'une turbomachine
FR3099787B1 (fr) * 2019-08-05 2021-09-17 Safran Helicopter Engines Anneau pour une turbine de turbomachine ou de turbomoteur
US11174754B1 (en) * 2020-08-26 2021-11-16 Solar Turbines Incorporated Thermal bridge for connecting sections with a large temperature differential under high-pressure conditions

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3975901A (en) * 1974-07-31 1976-08-24 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Device for regulating turbine blade tip clearance
US4752184A (en) * 1986-05-12 1988-06-21 The United States Of America As Represented By The Secretary Of The Air Force Self-locking outer air seal with full backside cooling
US5984630A (en) * 1997-12-24 1999-11-16 General Electric Company Reduced windage high pressure turbine forward outer seal
CN1269459A (zh) * 1999-04-01 2000-10-11 Abb阿尔斯通电力(瑞士)股份公司 燃气透平的隔热屏
US6200091B1 (en) * 1998-06-25 2001-03-13 Societe Nationale d'Etude et de Construction de Moteurs d'Aviation “SNECMA” High-pressure turbine stator ring for a turbine engine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3391904A (en) * 1966-11-02 1968-07-09 United Aircraft Corp Optimum response tip seal
BE756582A (fr) * 1969-10-02 1971-03-01 Gen Electric Ecran circulaire et support d'ecran avec dispositif de reglage de la temperature pour turbomachine
US3966354A (en) * 1974-12-19 1976-06-29 General Electric Company Thermal actuated valve for clearance control
US4177004A (en) * 1977-10-31 1979-12-04 General Electric Company Combined turbine shroud and vane support structure
FR2548733B1 (fr) * 1983-07-07 1987-07-10 Snecma Dispositif d'etancheite d'aubages mobiles de turbomachine
US4642024A (en) * 1984-12-05 1987-02-10 United Technologies Corporation Coolable stator assembly for a rotary machine
JP3302370B2 (ja) * 1995-04-11 2002-07-15 ユナイテッド・テクノロジーズ・コーポレーション 薄膜冷却スロットを備えたタービンブレードの外部エアシール
JPH10331602A (ja) * 1997-05-29 1998-12-15 Toshiba Corp ガスタービン
JP4269828B2 (ja) * 2003-07-04 2009-05-27 株式会社Ｉｈｉ シュラウドセグメント

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3975901A (en) * 1974-07-31 1976-08-24 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Device for regulating turbine blade tip clearance
US4752184A (en) * 1986-05-12 1988-06-21 The United States Of America As Represented By The Secretary Of The Air Force Self-locking outer air seal with full backside cooling
US5984630A (en) * 1997-12-24 1999-11-16 General Electric Company Reduced windage high pressure turbine forward outer seal
US6200091B1 (en) * 1998-06-25 2001-03-13 Societe Nationale d'Etude et de Construction de Moteurs d'Aviation “SNECMA” High-pressure turbine stator ring for a turbine engine
CN1269459A (zh) * 1999-04-01 2000-10-11 Abb阿尔斯通电力(瑞士)股份公司 燃气透平的隔热屏

Also Published As

Publication number Publication date
RU2435039C2 (ru) 2011-11-27
US20070071598A1 (en) 2007-03-29
CA2560227C (fr) 2013-09-10
JP4990586B2 (ja) 2012-08-01
RU2006133869A (ru) 2008-04-27
EP1775427B1 (fr) 2008-11-05
CA2560227A1 (fr) 2007-03-23
FR2891300A1 (fr) 2007-03-30
US7641442B2 (en) 2010-01-05
EP1775427A1 (fr) 2007-04-18
DE602006003502D1 (de) 2008-12-18
CN1936279A (zh) 2007-03-28
JP2007085346A (ja) 2007-04-05

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